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A B C D E F G H I J K L M N O P Q R S T U V W X Y Z ALL

A

  • Adaptive-neuro-fuzzy controller Design and Real-time Implementation of the Adaptive-Neuro-Fuzzy Controller for a Temperature Control System using Model-Based Design [Volume 10, Issue 4, 2017, Pages 9-17]

  • Amplitude and frequency of oscillation Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]

  • Artificial Neural Networks Satellite Orbit Prediction Through Observation Data and the Artificial Neural Networks [Volume 10, Issue 2, 2017, Pages 1-8]

  • Assumption of risk Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]

  • Atomization efficiency Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]

  • Atomization setup Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2017, Pages 1-7]

  • Attitude control of spacecraft Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]

  • Attitude determination Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]

  • AZMIN tool A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]

C

  • Combustion efficiency Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor [Volume 10, Issue 1, 2017, Pages 15-25]

  • Communication satellite HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2017, Pages 19-28]

  • Communication satellites A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]

  • Communication satellites GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]

  • Container Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]

  • Contribution of injured person Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]

  • Cyclone Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]

D

  • Damping baffles Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]

  • Decreased design time A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]

  • De-tumbling mode HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2017, Pages 19-28]

  • Differential electrical potential Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]

  • Differential flatness Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]

  • Dual throat nozzle 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]

  • Duty to mitigate Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]

  • Dynamic programming Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]

E

  • Earth station Plasma Antenna Technology in Space Missions [Volume 10, Issue 1, 2017, Pages 27-34]

  • Effervescent fuel Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]

  • Electricalpower subsystem HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2017, Pages 19-28]

  • Electrostatic discharge Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]

  • Emission indices Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor [Volume 10, Issue 1, 2017, Pages 15-25]

  • Energy-based model Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]

  • Estimator A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]

  • Experimental data Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]

  • Explicit guidance Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]

F

  • Floating electrical potential Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]

G

  • Genetic algorithm Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]

  • Geometrical analogy 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]

  • GEO orbit GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]

  • Geostationary orbit A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]

H

  • Hardware in loop HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2017, Pages 19-28]

  • Helmholtz coil Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]

  • Hydrazine monopropellant propulsion system Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results [Volume 10, Issue 2, 2017, Pages 53-63]

I

  • Inertial Navigation System A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]

  • International liability Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]

L

  • Launch abort system A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft [Volume 10, Issue 1, 2017, Pages 1-13]

  • Linear Quadratic Regulator Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]

  • Liquid sheet instability Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2017, Pages 1-7]

M

  • Magnetometer Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]

  • Mean droplet diameter Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]

  • Micro-turbine 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]

  • Model-based design Design and Real-time Implementation of the Adaptive-Neuro-Fuzzy Controller for a Temperature Control System using Model-Based Design [Volume 10, Issue 4, 2017, Pages 9-17]

  • Model-Free controller Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]

  • Multi beam satellite communication systems An Optimal Power Allocation in Multi-Beam Satellite Communication Systems Including Inter-Beam Interference by Particle Swarm Optimization (PSO) [Volume 10, Issue 1, 2017, Pages 55-60]

  • Multidisciplinary design optimization Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results [Volume 10, Issue 2, 2017, Pages 53-63]

N

  • Nonlinear attitude Control A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft [Volume 10, Issue 1, 2017, Pages 1-13]

  • Nonlinear Quadratic Tracking (NQT) Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]

  • Non-linear sloshing Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]

  • Numerical analysis Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]

O

  • On-off thruster actuator Robust Optimization of Satellite Attitude Control with Thruster Actuators based on Combined Objective Function [Volume 10, Issue 4, 2017, Pages 55-66]

  • Optimal guidance Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]

  • Optimal guidance Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]

P

  • Parametric models GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]

  • Partial Least Squares (PLS) Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]

  • Plasma antenna Plasma Antenna Technology in Space Missions [Volume 10, Issue 1, 2017, Pages 27-34]

  • Plasma array Plasma Antenna Technology in Space Missions [Volume 10, Issue 1, 2017, Pages 27-34]

  • Power allocation An Optimal Power Allocation in Multi-Beam Satellite Communication Systems Including Inter-Beam Interference by Particle Swarm Optimization (PSO) [Volume 10, Issue 1, 2017, Pages 55-60]

  • PSO optimization An Optimal Power Allocation in Multi-Beam Satellite Communication Systems Including Inter-Beam Interference by Particle Swarm Optimization (PSO) [Volume 10, Issue 1, 2017, Pages 55-60]

R

  • Reacting turbulent flow Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor [Volume 10, Issue 1, 2017, Pages 15-25]

  • Reentry Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]

  • Re-entry vehicles Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]

  • Regression Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]

  • Resonance Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]

  • Robustguidance Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]

  • Roll damping coefficient Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]

S

  • Satellite attitude control Robust Optimization of Satellite Attitude Control with Thruster Actuators based on Combined Objective Function [Volume 10, Issue 4, 2017, Pages 55-66]

  • Satellite Position Satellite Orbit Prediction Through Observation Data and the Artificial Neural Networks [Volume 10, Issue 2, 2017, Pages 1-8]

  • Separation Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]

  • Sequential design Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results [Volume 10, Issue 2, 2017, Pages 53-63]

  • Spacecraft Plasma Antenna Technology in Space Missions [Volume 10, Issue 1, 2017, Pages 27-34]

  • Spacecraft A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft [Volume 10, Issue 1, 2017, Pages 1-13]

  • Spacecraft charging Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]

  • Space law Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]

  • SPIS Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]

  • Spray cone Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2017, Pages 1-7]

  • Statistical design A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]

  • Statistical models GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]

  • Sun sensor Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]

  • Sun simulator Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]

  • Swirl injector Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]

  • Swirl injector Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2017, Pages 1-7]

T

  • Temperature control system Design and Real-time Implementation of the Adaptive-Neuro-Fuzzy Controller for a Temperature Control System using Model-Based Design [Volume 10, Issue 4, 2017, Pages 9-17]

  • Thrust vector control 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]

  • Time step Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]

  • TLE Satellite Orbit Prediction Through Observation Data and the Artificial Neural Networks [Volume 10, Issue 2, 2017, Pages 1-8]

  • Trapped vortex combustor Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor [Volume 10, Issue 1, 2017, Pages 15-25]

  • Turbulent Flow Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]

  • Two phase Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]

U

  • UAV A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]

  • Uncertainty Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]

  • Uncertainty Robust Optimization of Satellite Attitude Control with Thruster Actuators based on Combined Objective Function [Volume 10, Issue 4, 2017, Pages 55-66]

V

  • Validation GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]

  • Vision Navigation A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]

  • Volume of fluid technique Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]

W

  • Weber number Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]